COMBINED TURBOJET AND RAMJET ENGINE
    1.
    发明申请
    COMBINED TURBOJET AND RAMJET ENGINE 有权
    组合式涡轮发动机和RAMJET发动机

    公开(公告)号:US20130305686A1

    公开(公告)日:2013-11-21

    申请号:US13989070

    申请日:2011-11-14

    IPC分类号: F02K3/00

    摘要: A combined engine includes a turbopump including a pump injecting hydrogen into a heater arranged in an outer casing downstream from a central body, and a subsonic turbine driving the pump, which turbine receives partially-expanded hydrogen collected at an outlet from the heater to apply the hydrogen to a supersonic turbine to operate the engine as a turbojet. The hydrogen from the supersonic turbine is collected in tubes inside the central body to be sent to a combustion chamber defined downstream from the central body, while the hydrogen that is partially expanded in the subsonic turbine is sent directly to the combustion chamber via injectors to operate the engine as a ramjet.

    摘要翻译: 组合发动机包括涡轮泵,其包括将氢气注入布置在中心体下游的外壳中的加热器中,以及驱动泵的亚音速涡轮机,该涡轮机接收在加热器的出口收集的部分膨胀的氢气, 氢气到超音速涡轮机,以将发动机用作涡轮喷气发动机。 来自超音速涡轮机的氢气被收集在中心体内的管中,以被送到定义在中心体下游的燃烧室,而在亚音速涡轮机中部分膨胀的氢气通过喷射器被直接送入燃烧室以操作 发动机作为冲压式起重机。

    Combined turbojet and ramjet engine
    2.
    发明授权
    Combined turbojet and ramjet engine 有权
    组合式涡轮喷气发动机和冲压式发动机

    公开(公告)号:US09422889B2

    公开(公告)日:2016-08-23

    申请号:US13989070

    申请日:2011-11-14

    摘要: A combined engine includes a turbopump including a pump injecting hydrogen into a heater arranged in an outer casing downstream from a central body, and a subsonic turbine driving the pump, which turbine receives partially-expanded hydrogen collected at an outlet from the heater to apply the hydrogen to a supersonic turbine to operate the engine as a turbojet. The hydrogen from the supersonic turbine is collected in tubes inside the central body to be sent to a combustion chamber defined downstream from the central body, while the hydrogen that is partially expanded in the subsonic turbine is sent directly to the combustion chamber via injectors to operate the engine as a ramjet.

    摘要翻译: 组合发动机包括涡轮泵,其包括将氢气注入布置在中心体下游的外壳中的加热器中,以及驱动泵的亚音速涡轮机,该涡轮机接收在加热器的出口收集的部分膨胀的氢气, 氢气到超音速涡轮机,以将发动机用作涡轮喷气发动机。 来自超音速涡轮机的氢气被收集在中心体内的管中,以被送到定义在中心体下游的燃烧室,而在亚音速涡轮机中部分膨胀的氢气通过喷射器被直接送入燃烧室以操作 发动机作为冲压式起重机。

    RADIAL MAGNETIC BEARING AND METHOD OF MANUFACTURE
    3.
    发明申请
    RADIAL MAGNETIC BEARING AND METHOD OF MANUFACTURE 有权
    径向磁性轴承及其制造方法

    公开(公告)号:US20150137643A1

    公开(公告)日:2015-05-21

    申请号:US14517770

    申请日:2014-10-17

    IPC分类号: F16C32/04 B23P15/00 F16C43/04

    摘要: A radial magnetic bearing having an inner rotor including a central shaft having a ferromagnetic armature mounted on the shaft and an outer stator providing a plurality of electromagnets including poles made of ferromagnetic material which project radially inwardly towards the rotor is provided. As such, air-gaps (e) are left between end faces of the poles and the ferromagnetic armature, and coils wound around the poles. The poles are extended through outer portions attached to a supporting member. Each pole and the corresponding outer portion are included in an angularly segmented module providing a stack of laminations made of ferromagnetic material. The outer portion defines shoulders with respect to the corresponding pole, the outer portion contacting outer portions of neighboring segmented modules and the outer portions of all segmented modules being assembled by clamping rings, wherein the coils located in free spaces around the poles are mounted in a string.

    摘要翻译: 一种径向磁轴承,其具有内转子,该内转子包括具有安装在该轴上的铁磁衔铁的中心轴和设置多个电磁体的外定子,该多个电磁体包括由径向向内朝向转子突出的铁磁材料制成的极。 因此,气隙(e)留在磁极的端面和铁磁电枢之间,线圈缠绕在磁极上。 极通过附接到支撑构件的外部部分延伸。 每个极和对应的外部部分包括在角度分段的模块中,提供由铁磁材料制成的叠片。 外部部分相对于相应的极限定肩部,接触相邻分段模块的外部的外部部分和所有分段模块的外部部分由夹紧环组装,其中位于极周围的自由空间中的线圈安装在 串。

    Radial magnetic bearing and method of manufacture

    公开(公告)号:US09845829B2

    公开(公告)日:2017-12-19

    申请号:US14517770

    申请日:2014-10-17

    摘要: A radial magnetic bearing having an inner rotor including a central shaft having a ferromagnetic armature mounted on the shaft and an outer stator providing a plurality of electromagnets including poles made of ferromagnetic material which project radially inwardly towards the rotor is provided. As such, air-gaps (e) are left between end faces of the poles and the ferromagnetic armature, and coils wound around the poles. The poles are extended through outer portions attached to a supporting member. Each pole and the corresponding outer portion are included in an angularly segmented module providing a stack of laminations made of ferromagnetic material. The outer portion defines shoulders with respect to the corresponding pole, the outer portion contacting outer portions of neighboring segmented modules and the outer portions of all segmented modules being assembled by clamping rings, wherein the coils located in free spaces around the poles are mounted in a string.